Interface for cargo loaders

ABSTRACT

An interface system for cargo loaders which is especially suited for use with aircraft cargo loaders. The interface is secured to a deck structure forming part of the cargo loader. The interface system includes a primary interface member which can be extended or retracted with respect to the end of the deck. In addition to extension and retraction, the primary interface member can be angularly adjusted with respect to the end of the deck. In one embodiment a secondary interface member is stowed adjacent to the primary interface or nested within a recess formed in the primary interface. The secondary interface can be extended or retracted with respect to the primary interface member. The secondary interface can also be designed for angular adjustment. The primary interface also includes lateral extension members which can be varied in position to either decrease or increase the transverse length of the primary interface member. The flexibility in elongation, retraction and angular positioning of the interface system enables a loader to be used with a greater variety of cargo loading areas and is especially useful in adapting to the multitude of different aircraft cargo doors, especially those with recessed door sills.

This is a divisional of co-pending application Ser. No. 07/770,114 filedon Oct. 2, 1991, now U.S. Pat. No. 5,219,259 which is acontinuation-in-part of U.S. Ser. No. 07/594,146 filed Oct. 10, 1990 andnow U.S. Pat. No. 5,118,241.

BACKGROUND OF THE INVENTION

Field of the Invention

This invention relates to an interface for a cargo loader which includesmeans for adjusting to accommodate different size docking means andpositions. More specifically, this invention relates to an articulatinginterface especially suited for use with an aircraft cargo loader.

The commercial and military fleet of cargo aircraft is very diverse witheach airplane having one or more possible cargo compartments and loadingdoors. Because of the predominance of wide body aircraft in thetransport fleet, the tendency has been towards the development andfielding of large multipallet loaders having their own propulsion meansand powered container handling features.

Since many commercial and military cargo aircrafts can be loaded fromfront or rear doors, the loader body width has usually been made in theprior art of a width of 96, 108, or 125 inches to accommodate thevarious standard wide-body pallets and containers. However, many lowerdeck doors and access openings on relatively small aircraft are smallerin width than 96 inches (e.g., 60-90 inches).

Moreover, the prior art cargo loading equipment, used to access smalleraircraft doors recessed into the fuselage of the airplane, generallyconsisted of container lifts made narrow to fit the smaller openingsassociated with such aircraft cargo doors. Some prior art cargo liftsrequire that the containers be manually pushed on and pushed off thecargo loader. Thus, in addition to not being flexible enough to handlethe diverse range of aircraft loading and unloading cargo areas, suchprior art cargo loading equipment also require excessive handling inloading and unloading containers from an aircraft.

U.S. Pat. No. 3,944,096 illustrates an angularly adjustable, poweredinterface for use with a freight transporter and loader. The angularadjustment feature of the interface of U.S. Pat. No. 3,944,096 enablesthe operator to adjust the loader for accessing "behind the wing" cargodoors. U.S. Pat. No. 3,944,096, however, fails to provide access toaircraft cargo compartments of all recent wide and narrow body cargoaircraft and requires a high degree of user expertise in positioning theloader.

SUMMARY OF THE INVENTION

The present invention presents a solution to the above-noted problemsconcerning the lack of flexibility in the prior art aircraft cargoloaders and their inability to handle the diverse range of aircraftcargo openings. In addition, the present invention provides the requiredflexibility while also avoiding difficult operation procedures such thatan operator can easily handle the system and load and unload an aircraftat a relatively fast rate.

The following summary description is made in reference to an interfacesystem specifically adapted for use with an aircraft cargo loader. Thepresent invention can also be useful in association with other vehicleshaving similar requirements to that of an aircraft cargo loader.However, the present invention is especially suited for handling thediverse range of aircraft cargo access openings.

One embodiment of the interface system of the present invention includesa deck and a primary interface connected to the deck by way ofconnecting means. The connecting means for connecting the primaryinterface to the deck includes a first extension-retraction means forextending and retracting the primary interface with respect to the deck.The primary interface has a recess or a receiving area formed along oneof its sides which is dimensioned to receive, in stowable fashion, asecondary interface member. Alternatively, the secondary interfacemember may be retracted against the primary interface and stowedadjacent the primary interface without the use of a recess. In eithersituation it is preferable to have the upper surface of the primaryinterface essentially coplanar with the upper surface of the secondaryinterface. Also, when a recess is used, it is preferable to have therecess deep enough to place the front edge of the secondary interfaceessentially coplanar with the front edge of the primary interface. Therecess should also open into the upper surface of the primary interfacesuch that when the secondary interface is in its stowage position itsupper surface is coplanar with the primary interface.

The secondary interface member is secured to the primary interfacemember by way of securement means. The securement means includes asecond extension-retraction means for extending and retracting thesecondary interface with respect to the primary interface. The secondaryinterface can thus be stowed or nested away against or within theprimary interface and extended out away from the primary interface.

The primary interface includes a first outboard end and a secondoutboard end. The first extension-retraction means includes a firstextension-retraction member and a second extension-retraction member.The first extension-retraction member is secured to the primaryinterface closer to the first outboard end than to the second outboardend while the second extension-retraction member is secured to theprimary interface at a position closer to the second outboard end thanto the first outboard end. Furthermore, the first and secondextension-retraction members are pivotably connected to the primaryinterface and each extension-retraction member is individuallyextendable and retractable such that the primary interface can beangularly adjusted with respect to the deck by varying the amount ofextension and retraction of the first and second extension-retractionmembers.

In a preferred embodiment, the first and second extension-retractionmembers include a hydraulic cylinder, a tubular guide positionedadjacent the hydraulic cylinder and secured to the under surface of thedeck, a support arm slidingly received in the tubular guide, and abracket member. The bracket member is pivotably joined at one end to thehydraulic cylinder and pivotably joined at its other end to the supportarm. In addition, the bracket is secured to the primary interface.Alternatively, the hydraulic cylinder could be maintained within thetubular guide and tubular support arm. In either situation, when thehydraulic cylinder is extended for one extension-retraction member andthe hydraulic cylinder for the other extension-retraction member isretracted, the primary interface member is set at an angle with respectto the end edge of the deck. Preferably, the maximum angle amount isabout 15 degrees with respect to a center line extending parallel withthe end edge of the deck.

The primary interface also preferably includes a first lateral extensionpositioned at the first outboard end a second lateral extensionpositioned at the second outboard end. The first and second lateralextensions include pivotable connection means as well as means to lockthe lateral extensions into a first position wherein an upper surface ofthe lateral extensions is generally planar with an upper surface of theremaining main body portion of the primary interface and into a secondposition wherein the lateral extensions are locked in place below theupper surface of the main body portion of the primary interface. In thisembodiment, the lateral extensions pivot about a horizontal axis suchthat the lateral extensions pivot from an upper position to a positionbelow the main body portion of the primary interface. For example, byrotating downwardly two 15 inch lateral extensions positioned atopposite ends of the main body portion of the primary interface andlocking those lateral extensions, preferably along the underside of theprimary interface, a 92 inch wide primary interface can be reduced to 62inches. By designing the secondary interface to have a width of 60inches, the combination of the 62 inches and 60 inches interface membersenables use of the loader with respect to certain aircraft which requirethe primary interface to also be extended into the fuselage cutout oraccess opening. In fact, the door sill of the lower deck cargo doors ofcertain airplanes, such as that of a 747 or DC-10 aircraft, is recessedwithin the outer skin of the aircraft and some lower deck cargo doorsare only wide enough (about 65 inches) to take 60 inch wide containers.

Further, some aircraft have a wing fillet which makes the loading orunloading operation even more problematic. With aircraft having recesseddoor sills and/or wing fillets, the primary and secondary interfacesmust extend into the opening to reduce the gap over which the palletsand containers must pass.

If it was possible to extend the secondary interface without lowering orretracting the lateral extensions, the operator might extend the primaryinterface to reduce the gap and damage the skin and/or fairing of theairplane. Accordingly, as explained in greater detail below, means areprovided to monitor the positioning of the secondary interface andlateral extensions such that the lateral extensions are not extendedwhen the secondary interface is extended. With the secondary interfaceretracted, the primary interface can be extended with the lateralextensions outwardly extending so as to align the primary interface withwider door openings.

The invention also contemplates the use of one or more power rollerswhich are positioned on the primary interface. Means for drivinglyrotating the power roller or rollers is preferably attached to theprimary interface in a position below the under surface of the primaryinterface. A preferred embodiment also provides means for manipulatingthe power rollers either to a first position wherein the power rollersare above the upper planar surface of the primary interface and adaptedfor contact with cargo or to a second position wherein the power rollersare recessed so as to be flush with or below the upper planar surface ofthe primary interface. In addition to power rollers, nonpowered or idlerrollers can also be provided to assist in the conveyance of cargo loadsacross the extended interface. The idler rollers are preferably providedon the lateral extensions to assist in conveyance of cargo over theextremities of the primary interface. When the primary interface is setat an angle in one direction or another, the power rollers assist inturning the containers to the new direction of travel required foron/off loading.

The second extension-retraction means includes a first set of linkmembers and a second set of link members transversely spaced from oneanother. The first and second sets of link members each include a firstlink member pivotably secured to the primary interface and a second linkmember pivotably secured to the first link member at one end and to thesecondary interface at the other end. This arrangement enables thefolding of the secondary interface into the recess formed in the primaryinterface or into a position adjacent the front of the primaryinterface. The first and second sets of link members also each includereleasable locking means such as a locking pin extending through anaperture spaced from the common pivot point of the two link members. Thesecondary interface preferably is provided with at least one roller toassist in the conveyance of cargo across the interface and onto thedeck.

The invention further contemplates providing the secondary interfacewith a powered roller or rollers. In addition, rather than relying onthe link members, the secondary interface can be mounted to the primaryinterface in a manner similar to the arrangement used to secure theprimary interface to the deck structure. The latter arrangement providesfor even a greater degree of angular adjustment as both the primary andsecondary interfaces can be angularly adjusted.

The invention also contemplates the use of spring loaded rollers and aplurality of bumpers placed serially across the front end edge of thedeck. The spring loaded rollers are designed to retract into a recessformed in the edge of the deck whenever the primary interface is inabutment with the end of the deck. Once the primary interface isextended the spring loaded rollers extend into a position to assist inthe conveyance of cargo between the primary interface and the deck.

In one embodiment of the invention, a safety feature is provided suchthat whenever the secondary interface is extended from its stowedposition, the primary interface is precluded from being extended untilthe two lateral extensions have been rotated down and locked in place.Accordingly, detection means is relied upon both to determine whetherthe secondary interface is in an extended position and whether thelateral extensions are in an up or down position. Preferably, thedetection means is in communication with control means for controllingthe electrical or fluid input to the first extension-retraction means soas to enable either the activation or deactivation of the firstextension-retraction means. If the detection means determines that thesecondary interface is in an extended position and a lateral extensionis still in an up position, than the detection means will signal thecontrol means to deactivate the first extension-retraction means suchthat the primary interface cannot be extended. Alternatively, amechanical latch in the lateral extensions can be provided to preventextension of the secondary interface with the lateral extensions in anup position; and, conversely, to prevent the raising of the lateralextensions with the secondary interface extended.

An additional contemplated feature of the present invention is theinclusion of a pair of notched passageways in the primary interface anda pair of covers which can be releasably secured in the notchedpassageways. The notched passageway include tine ways for facilitatingthe positioning of fork lift tines during the removal and loading ofcontainers at the front of the loader by means of a forklift or similardevice.

In yet another embodiment of the invention, the first and secondextension-retraction means are positioned in spaced relationship withrespect to one another and each has a first end supported by the deck ofthe cargo loader. An interface assembly is secured to the second end ofthe first and second extension-retraction means. The interface assemblyincludes a main body with an upper and a lower surface and a first and asecond end. The first end of the main body is pivotably secured to thesecond end of the first extension-retraction means and the second end ofthe main body is pivotably secured to the second end of the secondextension-retraction means.

The embodiment further includes first and second lateral extensionsextending off of the first and second ends of the main body. The firstlateral extension member has a first end pivotably secured to the firstend of the main body such that the first end of the first lateralextension is free to pivot about an axis which extends between the upperand lower surface of said main body (e.g. vertical axis). The secondlateral extension has a first end pivotably secured to the second end ofthe main body. The first end of the second lateral extension also pivotsabout an axis which extends between the upper and lower surface of themain body.

First locking means is provided for locking the first lateral extensionin an extended position wherein the first lateral extension extends outaway from both the first and second extension-retraction means. A firstlocking member is also positioned on the first lateral extension forengagement with a spring driven pin supported by the main body when thefirst lateral extension is to be fixed in a retracted position. In theretracted position, the first lateral extension extends out away fromthe first extension-retraction means and towards the secondextension-retraction means. The first lateral extension is also spacedfrom and parallel to the front end of the main body.

Second locking means is also provided for locking the second lateralextension in an extended position wherein the second lateralextension-retraction means extends out away from both of the first andsecond extension-retraction means. A second locking member is alsopositioned on the second lateral extension for engagement with a springdriven pin supported by the main body when the second lateral extensionmember is to be placed in a retracted position. In the retractedposition, the second lateral extension extends out away from the secondextension-retraction means and towards the first extension-retractionmeans and has a front surface which is essentially coplanar to the frontsurface of the retracted first lateral extension and parallel withrespect to the front face of the main body.

Each of the first and second lateral extensions in this embodimentinclude a support beam. The first and second lateral extensions alsoeach include at their first end a bracket member extending transverse tothe support beam and a pivot pin secured to the main body and pivotablysecured to the bracket member on one side of the support beam. The firstand second locking means each further comprise disengageable engagementmeans supported by the bracket member on the other side of the supportbeam. The engagement means releasably fixes the lateral extensions inthe extended position. The preferred embodiment also includes exteriorroller assemblies positioned on each of the lateral extensions. Theroller assemblies include rollers and releasable locking means. Thereleasable locking means, when engaged, lock the rollers in a raisedposition (above the upper surface of the main body) and when disengagedresult in the rollers being lowered below the upper surface of the mainbody.

The present invention further comprises interior roller assemblies(e.g., two pairs) which include rollers and releasable locking means.The releasably locking means, when engaged, position the rollers in araised position and, when disengaged, result in the rollers beinglowered below the upper surface of the main body. External rollerspositioned on one side of the support beams of the lateral extensionsare spaced such that their axis of rotation is essentially aligned withthe axis of rotation of interior rollers supported by the front of themain body when the lateral extensions are in the retracted position.

The disengageable engagement means of the preferred embodiment includesa cylinder which is supported by the bracket member and has a slotextending axially along the cylinder. A pair of engagement pins arepositioned within the cylinder and include gripping means which extendthrough the slot. A spring is positioned within the cylinder and betweenthe engagement pins so as to bias the pins outwardly towards andpartially out past the open ends of the cylinder. The gripping meansabut the ends of the slot so as to limit the amount the pins extend outpast the open ends of the cylinder. Holes or recesses are provided inupper and lower flanges forming part of the lateral extension brackets.Holes or recesses are also provided in upper and lower plates of themain body. The holes in the upper and lower plates are aligned with theholes in the flanges such that the outwardly biased pins extend throughthe flange holes and recesses or holes provided in the brackets of thelateral extensions. With the pins extending through the flange and intothe plate the lateral extensions are locked in their extended position.The gripping means allows a person to squeeze the pin members towardsthe center of the cylinders so as to release the pin members fromengagement with the apertures or holes formed in the main body. Thelateral extension can then be rotated 180° into their retractedposition. The present invention also contemplates utilizing automatic(e.g., electromechanical) disengageable mechanical means.

The embodiment further comprises a powered roller assembly supported bythe main body. The powered roller assembly including rollers and meansfor driving those rollers. The powered roller assembly includes meansfor raising the rollers to a position above the upper surface of themain body and into a position below the upper surface of the main body.

The first and second extension-retraction means of this embodimentpreferably each include an elongated arm and a hydraulic memberconnected at one end to the arm and at an opposite end to the desk. Thefirst and second arms are independently extendable and retractable awayand towards the deck with the hydraulic members. One set of the upperand lower plates of the main body includes slots and the arm of thecorresponding extension-retraction means extends in between the upperand lower plates and is slidingly fixed within the slot such that thearms are extendable away from the deck for different lengths so as toangle the main body.

The main body of the present invention includes a central axis extendingbetween the first and second ends of the main body and the locking meansare dimensioned and arranged such that the lateral extensions extend outessentially along the central axis of the main body when in the extendedposition and extend inwardly along an axis spaced and parallel to thecentral axis of the main body when the lateral extensions are in theretracted position.

The locking means for fixing the lateral extensions in place aredimensioned and arranged such that the lateral extensions pivotessentially 180° in passing between the extended position and theretracted position.

The extension-retraction means of the preferred embodiment includesliding means for sliding the arms within an elongated recesses formedin the deck. The arms and the corresponding recesses are dimensioned andarranged so as to limit the movement of the arms to sliding travelsolely along the central axis of the elongated recesses. The arms thusstay transverse to the front end of the deck and angling of the mainbody is achieved by extending one arm further than the other whileallowing one of the two arms to slide within the slots formed in theupper and lower plates.

Another embodiment of the present invention features an interface systemwhich includes a deck structure and first and secondextension-retraction means supported by the deck structure. A primaryinterface is supported by the first extension-retraction means such thatthe primary interface is movable by the first extension-retraction meansbetween an extended position away from the deck structure and aretracted position closer to the deck structure. A secondary interfaceis supported by the second extension-retraction means such that thesecondary interface is movable between an extended position away fromsaid deck and a retracted position closer to the deck structure.

The first extension-retraction means includes a first primary armconnected at one end to the primary interface and a second primary armconnected at one end to the primary interface. The first primary arm islaterally spaced from the second primary arm. The secondextension-retraction means includes a first secondary arm connected atone end to the secondary interface and a second secondary arm connectedat one end to the secondary interface and laterally spaced from thefirst secondary arm.

The embodiment further includes first interplay means forinterconnecting the primary arm and the first secondary arm andcoordinating the movement of the first primary arm and the secondprimary arm. Second interplay means is also provided for interconnectingthe second primary arm and the second secondary arm and coordinating themovement of the second primary arm and second secondary arm. The firstand second interplay means are dimensioned and arranged such that, whenthe first and second primary arms of the first extension-retractionmeans are extended and retracted, the extension and retraction of thesecond extension-retraction means is coordinated so that the secondaryinterface is maintained intermediately positioned between a front edgeof the deck structure and the primary interface.

The interface system of this embodiment has the primary and secondaryinterfaces each including a slotted recess with the first primary armbeing slidably received within the slotted recess formed in the primaryinterface and the first secondary arm slidably received within theslotted recess formed in the secondary interface.

The first and second extension-retraction means are dimensioned andarranged such that uneven extension of one of the primary arms resultsin a tilting of the primary interface, and the first and secondinterplay means are dimensioned and arranged such that, when the primaryinterface is tilted, the secondary interface is tilted by essentiallyone-half the angle of tilt of the primary interface.

The first and second interplay means each include a pair of sprocketsspaced along a respective secondary arm, a belt or chain in frictionalcontact around the pair of sprockets, means for connecting an adjacentprimary arm to the belt or chain, and means to connect the belt or chainto the deck structure.

The secondary interface also includes at least one through-area and theprimary arms are positioned laterally inside of the secondary arms so asto extend through the through-area or through-areas provided in thesecondary interface and so as to be in frictional contact with thesecondary interface. A preferred embodiment has the secondary interfaceformed as a rectangular frame structure with the primary arms extendingwithin the interior of the rectangular frame structure.

BRIEF DESCRIPTION OF THE FIGURES

FIG. 1 shows a perspective view of a transport loader with oneembodiment of the interface system attached therewith;

FIG. 2 shows a cut-a-way view of the front end of the transport loader'sdeck as well as a cut-a-way view of an aircraft cargo door;

FIG. 3 shows a front end view of the interface system shown in FIG. 2;

FIG. 4 shows a cut-a-way planar view of the interface system shown inFIG. 2 with both the primary interface and secondary interface in aretracted position;

FIG. 5 shows a cut-a-way planar view of the interface system shown inFIG. 2 with the primary interface and secondary interface in an extendedposition and, as exemplified by dashed lines, the primary and secondaryinterface set at an angle with respect to the end edge of the deck;

FIG. 5A shows a planar, cut-away view of the interface system having amodified securement means securing the secondary interface to theprimary interface;

FIG. 6 shows a planar cut-a-way view of an outboard end of the primaryinterface with the lateral extension locked in an extended position;

FIG. 6A shows an elevational, cut-away view of an outboard end of theprimary interface having an unlocked and partially rotated lateralextension;

FIG. 6B shows the arrangement of FIG. 6A except for the lateralextension being fully rotated and locked into a second position belowthe main body portion of the primary interface;

FIG. 7A shows a planar cut-away view of the interface system being usedwith an airplane having a recessed door sill;

FIG. 7B shows a planar cut-away view of the interface system havingangularly adjustable primary and secondary interfaces in operation withrespect to an airplane having a recessed door sill and a wing fillet;

FIG. 8A shows a planar, cut-away view of the outboard end of the primaryinterface which has a notched passageway formed therein;

FIG. 8B shows a perspective view of a cover insertable within thenotched passageway;

FIG. 8C shows an elevational view of the cover in position within thenotched passageway;

FIG. 9 shows, in cut-away, a perspective view of the powered rollers ofthe present invention;

FIG. 10 shows a partially cut-away, planar view of a mechanical latchassembly suitable for preventing extension or retraction of thesecondary interface;

FIG. 11 shows a perspective view of another embodiment of the inventionin stowage mode with respect to a supporting deck and with lateralextensions fully suspended;

FIG. 12 shows the interface system of FIG. 11 with the deck structureremoved for clarity;

FIG. 13 shows a top plan view of the interface assembly shown in FIG. 12with the lateral extensions retracted;

FIG. 14 shows a top plan view of that which is shown in FIG. 12;

FIG. 15 shows a front elevational view of that which is shown in FIG.12;

FIG. 16 shows a side elevational view of that which is shown in FIG. 15;

FIG. 17A illustrates a lock pin assembly;

FIG. 17B illustrates one of the lock pins of the lock pin assembly shownin FIG. 17A;

FIG. 18A shows a cut-away view taken along Z--Z in FIG. 12;

FIG. 18B shows a cut-away view taken along line X--X in FIG. 13;

FIG. 19A shows a planar view of another embodiment of the presentinvention;

FIG. 19B shows a side view of that which is shown in FIG. 19;

FIG. 20 shows a planar view of that which is shown in FIG. 19A exceptwith the upper portion of the deck structure removed for clarity;

FIG. 21 shows a planar, cut-away view of the extension-retraction meansand interplay means for the interface assembly;

FIG. 22 shows a cross-sectional view taken along line II--II in FIG. 21;

FIG. 23 shows a cross-sectional view taken along line III--III in FIG.21;

FIG. 24 shows a planar view like that of FIG. 20 except with theinterface assembly at maximum extension;

FIG. 25 shows the same view as in FIG. 24 except with the primary andsecondary interface at a maximum angle orientation; and

FIG. 26 shows a schematic illustration of the general principle lyingbehind the coordinated movement of interface 1012 and 1014.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

FIG. 1 shows a perspective view of an aircraft transport loader 100having a base frame 102 supported by a set of steerable wheels 104 and aset of driving wheels 106. Main lift assembly 108 is secured to theunder structure of deck 110. Deck 110 has operator's cab 112 secured onthe left-hand side edge of deck front end 114.

Positioned at the forward edge of deck front end 114 is interface system116.

FIG. 2 illustrates interface system 116 positioned between a cargo doorframe 118 and deck 110. As there shown, primary interface 120 ispositioned between aircraft door 118 and deck 110 from which it issupported. Deck 110 is shown to have a front edge 122 and both powerrollers 124 and idler rollers 126 positioned along the deck's upperconveying surface. Deck 110 further includes spring loaded rollers 128and bumpers 130.

Primary interface 120 includes support arms 132 and 134 which aresecured in a sliding relationship to the under surface of deck 110. Asshown in FIG. 2, by extending support arm 132 further out away from thefront edge 122 of deck 110 than extension support arm 134, an angledorientation of primary interface 120 relative to the deck is possible.FIG. 2 further illustrates secondary interface 136 in its stowedposition wherein secondary interface 136 is received within acorresponding recess or cutout formed in the front of primary interface120. Secondary interface 136 can include idler rollers 138 while primaryinterface 120 features powered rollers 140 as well as its own idlerrollers 142 and 144. Idler rollers 142, 144 are preferably positioned onthe outboard ends of primary interface 120 and, more preferably, on theupper surface of lateral extensions 146 and 148 which extend outwardlyoff of main body portion 150.

FIG. 3 shows a front end view of interface system 116. As there shown,lateral extensions 146 and 148 are pivotably connected to main bodyportion 150 at hinge locations 152, 154, respectively. Positioned underpower rollers 140 is power means 156 which includes an appropriatedriving source such as an electric motor or hydraulic motor 158 togetherwith an appropriate gearing or pulley system 160. FIG. 3 also revealssensors 162 and 164 the purpose for which is discussed further below.

FIG. 4 illustrates a planar view of interface system 116 as well as acut-a-way portion of deck 110. As shown in FIG. 4, a plurality of springrollers 128 extend out from front edge 122 of deck 110 towards theinside surface of primary interface 120. Spring loaded rollers 128 areadapted for compression situations such as where primary interface 120is retracted against bumpers 130. Support arms 132 and 134 are shownslidingly received within guide extension channel members 166 and 168which can be supported by the under surface of deck 110. Hydrauliccylinders 170 and 172 are shown positioned adjacent guide extensionchannel members 166, 168. Hydraulic cylinders 170 and 172 can also besecured to the under structure of deck 110. FIG. 4 further illustratessecondary interface 136 as well as the extension-retraction means forthe secondary interface which comprises link assemblies 174 and 176. Asshown in FIG. 4, each link assembly includes a pair of link membersadapted to be placed in a folded arrangement when secondary interface136 is nestled within cutout 178 formed in primary interface 120.

FIG. 5 illustrates in planar view both secondary interface 136 andprimary interface 120 in an extended position with respect to deck 110.FIG. 5 further illustrates, in dashed lines, the maximum angleadjustment made possible by extending one extension member to a greaterextent than the other. FIG. 5 shows support arms 132 and 134 extendingout away from front edge 122 of deck 110. The extension of support arms132 and 134 is made possible by extending rods 180 and 182 which form apart of hydraulic cylinders 170 and 172 (FIG. 4). The ends of rods 180and 182 are pivotably connected to brackets 184 and 186. Brackets 184and 186 also include means for pivotably securing the forwardmost endsof support arms 132 and 134. In addition, bracket members 184 and 186are secured to main body 150 of primary interface 120. The pivotalrelationship between brackets 184, 186 and corresponding cylinder rods180 and 182 as well as the pivotal relationship between brackets 184,186 and extension support arms 132 and 134 makes it possible for angleadjustments to be made to the primary interface 120 as illustrated inthe dashed lines in FIG. 5. The maximum angle of adjustment isrepresented by angle X which in a preferred embodiment is about 15degrees. Although primary interface 120 is shown angled towards theright front end of deck 110, a similar angle adjustment can be made inan opposite, counterclockwise, direction. The notched recesses providedat the ends of lateral extensions 146 and 148 avoids premature abutmentwhen primary interface is being angularly adjusted. Theextension-retraction means between primary interface 120 and deck 110and the extension-retraction means between primary interface 120 andsecondary interface 136 each preferably has a maximum extension of aboutone foot.

FIG. 5 illustrates link assemblies 174 and 176 which each include afirst link member 188 and a second link member 190 at the other end.Link members 188 are pivotably connected to primary interface 120 at oneend and to a corresponding link member 190 at their other end. Linkmembers 190 are secured at their other end to secondary interface 136*.Link members 188 and 190 can be locked in an extended position byappropriate locking means such as a locking pin extending through anaperture being in both link members 188 and 190 with the aperture formeda short distance away from the pivot connection between link members 188and 190. FIG. 5 also illustrates sensor 192 the purpose for which isdescribed further below.

FIG. 5A illustrates an alternate embodiment of the invention whereinsecondary interface 136' is positioned adjacent primary interface 120'.The elements in common with those shown in FIG. 4 have been designatedwith equivalent dashed numbers. FIG. 5A further reveals the replacementof link assemblies 174 and 176 with a hydraulic system featuring a righthydraulic assembly 300 and a similar left hydraulic assembly (notshown). Hydraulic assembly 300 includes tubular guide 301 and slidemember 302 slidingly received within tubular guide 301. Slide member 302is pivotably attached at 307 to pivot support 303 which is attached tosecondary interface 136. Pivot support 303 is also pivotably attached torod 305 of hydraulic member 306. Hydraulic member 306 is preferablysecured to the under surface of primary interface 120'.

FIG. 5A also illustrates rollers 308 in secondary interface 136' whichare preferably powered either by a source attached to the under surfaceof secondary interface 136' (not shown) or through the same drivingmeans used for powered rollers 140 which is shown in FIG. 9 anddiscussed further below.

FIGS. 6, 6A and 6B illustrate lateral extension 148 in pivotalconnection with main body portion 150 of primary interface 120. Thepivotal relationship between lateral extension 148 and main body portion150 is made possible by hinge connection 154. As it is required toreduce the transverse width of primary interface 120 for certainaircraft cargo door frame sizes, lateral extension 148 is madepositionable in one of two locations. The first location is when thelateral extensions extend outwardly as shown in FIG. 3-5 and FIG. 6. Thesecond location is when the lateral extensions are locked in the mannerillustrated in FIG. 6B.

As further shown in FIGS. 6, 6A and 6B, lateral extension 148 is formedwith a plurality of upper insert members 310. Main body portion 150 hasformed therein a plurality of upper recesses 311 for receiving insertmembers 310. Recesses 311 are defined by upper extensions 312 formed atthe end of main body portion 150. Both upper extensions 312 and upperinsert members 310 have an aperture formed therein for receipt of pin313 when insert members 310 are received within recesses 311. FIG. 6illustrates the arrangement wherein pin 313 locks insert members 310 inposition within recesses 311.

Locking pin 313 is connected to main body portion 150 by lanyard 314.Positioned at the end of locking pin 313 is a pair of spring biasedlocking balls 315, 316 which prevent locking pin 313 from inadvertentlysliding out from a locking position.

FIG. 6A illustrates the unlocking of insert members 310 from recesses311 and rotation of lateral extension 148 to an intermediate positionbetween the first locking position as shown in FIG. 6 and the secondlocking position as shown in FIG. 6B.

FIGS. 6A and 6B illustrate lower insert members 317 (one shown) whichare received in lower recesses 318 in a manner similar to that describedfor the first locking position. As shown in FIG. 6B, once lower inserts317 are inserted within recesses 318 and the apertures in each arealigned, pin 313 can be inserted to fix lateral extension 136 in thesecond locking position.

FIG. 6A also shows sensor 164 which detects whether lateral extension148 is in the first or second locking position. As previously noted, ina preferred embodiment, if secondary interface 136 is in its extendedposition, primary interface 120 can only be extended out away from deck110 when lateral extensions 146 and 148 are in the second lockingposition below main body portion 150. Sensor 164 thus provides anindication that lateral extension 148 is in its proper position suchthat hydraulic cylinder 172 can be extended. A similar arrangement isprovided on the opposite side. Sensor 192 shown in FIG. 5 provides ameans to determine whether secondary interface 136 is extended orremains in a stowage position. Various other means for releasablylocking lateral extension 146 and 148 in the first and second lockingpositions are also contemplated although the above described arrangementis preferred.

FIGS. 7A and 7B illustrate an extended primary interface 120 withlateral extensions 146 and 148 in the second locking position and anextended secondary interface 136. More particularly, FIG. 7A illustratesthe relationship between interface system 116 and the lower deck cargodoor 320 of aircraft 321, such as a 747 or a DC-10 aircraft, recessedwithin the outer skin of the aircraft. FIG. 7B illustrates an aircrafthaving a wing fillet 322 with a recessed area for access to cargo door320. Detectors 162 and 164 would prevent extension of secondaryinterface 136 until after lateral extensions 146 and 148 are placed inthe second locking position. If it was possible to extend secondaryinterface 136 without lowering lateral extensions 146 and 148, then theoperator could inadvertently extend primary interface 120 to reduce thegap and damage the skin and/or fillet of the aircraft. With thesecondary interface retracted, however, it is possible to extend theprimary interface with lateral extensions 146, 148 in the first lockingposition such that primary interface 120 can be aligned with wider dooropenings of the aircraft such as the 104 inch cargo door in FIG. 2. FIG.7B also illustrates the use of extension-retention members such as thoseshown in FIG. 5A to secure the secondary interface to the primaryinterface such that the secondary interface can be varied in angularposition with respect to the primary interface. In a preferredembodiment both the primary and secondary interface can be angularlyadjusted. The present invention also contemplates making only one of thetwo interfaces angularly adjustable.

FIG. 8A illustrates notched passageway 208 formed in main body portion150 of primary interface 120. A notched passageway, similar to notchedpassageway 208, is provided on the opposite side of power rollers 140and is spaced to match the transverse spacing of forklift truck tines.These notched passageways enable the operator of a forklift truck toeasily slide the forklift tines between a heavy cargo container and theupper surface of the primary interface so as to facilitate the droppingoff or picking up of a container.

FIG. 8B illustrates cover 330 with protrusions 331 positioned forreleasably retaining cover 330 in position within notched passageway 148as shown in FIG. 8C. With cover 330 in position an essentially completeupper planar surface is provided so as to facilitate manual sliding ofcontainers along the upper surface of primary interface 120. Covers 330are removed and stored when the notched passageways are in use.

FIG. 9 illustrates power rollers 140 removed from their recessedposition within main body portion 150 for the sake of clarity. As shown,power rollers 140 include a shaft 350 which is received at its endswithin bearing support members 351 and 352. Bearing support member 351is slidingly retained within grooved blocks 353 and 354. Likewise,bearing support member 352 is slidingly retained within grooved blocks355 and 356. Hydraulic means 357 (one shown) are positioned belowbearing support members 351 and 352 for enabling variations in theheight of the upper surface of the rollers with respect to main bodyportion 150.

Driving means M, which could include an electric or hydraulic motorcoupled with engagement means is drivingly engaged with shaft 152. Toretain driving means M in position while rollers 140 are varied inheight, bracket support 358 is secured at its ends to bearing supportmembers 351 and 352. Preferably, power rollers 140 are adjustable to afirst position wherein an upper surface of power rollers 140 is abovethe upper surface of main body portion 150 and into a second positionwhere the upper surface of power rollers 140 is either flush or belowthe upper surface of main body portion 150. A similar arrangement asthat described above could be utilized for driving rollers 308 in FIG.5A.

FIG. 10 shows a partially cut-away, planar view of the mechanical latchassembly 700 supported within primary interface 120. Mechanical latchassembly 700 includes first preventing means 702 which comprises cavity704 and pin member 706 biased outward by spring 708. Spring 708 isattached to flange 710 at one end and to a wall of cavity 704 at theother end. When a lateral extension (e.g., 148) is in an up position,pin member 706 is forced inwardly into reception means 712 which issecured to secondary interface 136. When lateral extension is placed ina down position, spring 708 forces pin 706 outwardly and out ofengagement with reception means 712 leaving secondary interface free forextension.

Reception means 712 is received within recess 714 forming part of secondpreventing means 716 which also includes spring member 718 and platemember 720. When lateral extension 148 is down and secondary interface136 is extended, plate 720 is biased forward to fill a portion of therecess and prevent pin member 706 from engaging with reception means712.

FIG. 11 shows a cut-away perspective view of another embodiment of thepresent invention which features interface system 520. Interface system520 includes deck 522 having front end 524, upper surface 526, and lowersurface 528. Deck 522 also features a stowage compartment 530 which isdimensioned to receive within its confines interface assembly 532 whilethe below described lateral extensions are extended.

Interface assembly 532 includes main body 534, upper surface 536 andlower surface 538. Main body 532 also includes first end 540 and secondend 542.

Extending outwardly away from first end 540 of main body 534 is firstlateral extension 544. First lateral extension 544 is comprised ofsupport beam 552 which is joined to bracket member 554. As illustrated,bracket 554 is C-shaped in cross section and extends transversely at theinterior end of support beam 552 to opposite sides of support beam 552.As further shown in FIG. 11, first lateral extension 544 includes afirst interior end 546 and a second exterior end 548.

Second lateral extension 556 extends out away from second end 542 ofmain body 534. Second lateral extension 556 features support beam 564which is joined at a first end 558 to bracket member 566. Bracket member566 extends to opposite sides of support beam 564. Bracket members 554and 566 are pivotably secured to main body 534 in a manner described inmore detail below.

FIGS. 11 and 12 illustrate lateral extensions 544 and 556 in theirextended position. First lateral extension 544 is fixed in its extendedposition by way of first locking means 568. Second lateral extension 556is fixed in its extended position by way of second locking means 578.

With reference to FIGS. 11, 12, 17a, 17b, 18a, and 18b, the function offirst and second locking means 568, 578 is provided below. As shown inFIG. 11, first lateral extension 544 has its bracket member 566pivotably secured between upper plate 547 and lower plate 549 of mainbody 534 by way of pivot pin 570. As shown in FIGS. 18A and 18B, pivotpin 570 extends through both upper flange 557 and lower flange 555 ofbracket member 554. Also, pin 570 extends into aligned holes or recessesformed in upper plate 547 and lower plate 549 and is preferably fixed atits ends to the upper and lower plates 547 and 549. FIGS. 18A and 18Balso illustrate first locking means 568 which includes disengageableengagement member 572 and the aforementioned pivot pin 570. Support beam552 of first lateral extension 544 extends transversely out away frombracket member 554 and includes an upper and lower shoulder toaccommodate upper and lower flanges 555 and 557 (see FIG. 11). Supportbeam 552 is positioned mid-way between disengageable engagement member572 and pivot pin 570 along bracket member 554.

FIGS. 17A and 17B illustrate in greater detail disengageable engagementmember 572 shown in FIGS. 18A and 18B. FIG. 17A illustratesdisengageable engagement member 572 as including cylinder 588 fixedlyretained between flange members 555 and 557. Cylinder 588 includes anaxially extending slot 600 extending from the exterior of cylinder 588into the hollow interior of cylinder 588. Engagement pin 602 and 603 aredimensioned and arranged so as to axially slide within the hollowinterior of cylinder 588 as well as the aligned holes formed in flangemembers 555 and 557. Also, when the disengageable engagement member 572is in an engaged state, engagement pins 602 and 603 extend through thealigned holes formed in upper plate 547 and lower plate 549. Theexternal ends of engagement pin 602 and 603 are beveled for easyinsertion with the aligned holes in the upper and lower plates. Spring606 is positioned between the interior ends of engagement pin 602 and603 and biases engagement pin 602 and 603 in an outward direction.Engagement pins 602 and 603 also feature gripping means 604 and 605extending away from the exterior of engagement pin 602 and 603 anddesigned for extension through slot 600.

In a preferred embodiment, gripping means 604 are bolts threaded intothe side of engagement pin 602 and 603 near the interior end of theengagement pins. Disengageable engagement member 572 is thus arrangedsuch that gripping means 604 and 605 can be drawn towards one anotheragainst the force of spring 606 so as to remove the exterior ends ofengagement pins 602 and 603 from engagement with upper and lower plates547 and 549. This action releases lateral extension 544 such that it maybe pivoted from its extended position to a retracted position asexplained in greater detail below. The arrangement for locking inposition second lateral extension 556 is the same as that for firstlateral extension 544 and thus further description would be redundant.

FIG. 13 illustrates lateral extensions 544 and 556 in their retractedposition and FIG. 14 illustrates the lateral extensions in theirextended position. A discussion of the movement of the lateralextensions between their retracted and extended position will be madewith regard to first lateral extension 544 only as the positioning andmovement of the second lateral extension 566 is essentially the samewith respect to the surrounding upper and lower plate and second end ofmain body 534. As shown in FIG. 13, when first lateral extension 544 isin its retracted position, bracket 554 extends out away from the frontend of plates 547 and 549. The rear end of bracket 554 is retained infixed relationship with respect to plate members 547 and 549 by way ofpivot pin 570. Pivot pin 570 forms a component of the aforementionedlocking means 568. As noted above, the forward most end of bracketmember 554 includes disengageable engagement means 572 which in FIG. 13is shown in its unengaged state such that pin 602 extends out abovebracket member 554 (see FIG. 18A taken along line X--X in FIG. 13). Inthe retracted position, support beam 552 is positioned so as to extendin front of main body 534 with its second end 548 directed towardssecond end 542 of main body 534. The support beam is spaced from theforwardmost end of plate 547 a distance equal to about 1/4 of the totalbracket length. Also, main body 534 includes a central, forward recess648 from which beam 552 is even further spaced. Also, support beam 552extends essentially parallel to the central axis of main body 534 whichextends between ends 540 and 542.

When lateral extensions 544 and 556 are in their retracted position,interface system 520 is well suited for the loading and unloading ofcargo in smaller width cargo areas, such as the smaller cargo bays foundon some aircraft. To maintain lateral extensions 544 and 556 in theirretracted position, a lock assembly is relied upon. There is a lockassembly associated with each of the lateral extensions. As shown inFIGS. 11, 12 and 15 each lock assembly includes a protruding first lockmember 574, 584 which, in a preferred embodiment, constitutes aforwardly extending plate secured to one side of a corresponding supportbeam 552, 564. Each lock assembly also comprises housings 576 and 586with internally spring-loaded engagement pins 577 and 579 located on thefront face of main body 532. With reference to FIG. 14, housings 576 and586 are positioned such that pins 577 and 579 engage with correspondingholes formed in first lock members 574 and 584 when the lateralextensions are retracted. Pins 577 and 579 also preferably featuregripping means (not shown) for achieving disengagement of pins 577 and579 from plates 574 and 584. Alternatively, pins 577 and 579 can bemechanically or electronically driven by, for example, a solenoid.

When it is desirable to use the interface system 520 for relativelylarge cargo bays, first and second lateral extensions 544, 556 are movedfrom their retracted position (FIG. 13) to their extended position (FIG.14). In so doing, pins 577 and 579 are shifted out of engagement withlock members 574, 584. Lateral extensions 544 and 556 are then shiftedessentially 180° about their respective pivot axis (central axis ofpivot pins 570 and 580) so as to be in the position illustrated in FIG.14.

To maintain lateral extensions 544 and 556 in an extended position, thedisengageable engaging means of each lateral extension (e.g. 572 in FIG.18a) is activated so as to have the outwardly extending pins (e.g. 602and 603, FIG. 18a) extend through the upper and lower plates (e.g. 547and 549) and lock the lateral extension in their extended positions.

FIGS. 13 and 14 also illustrate first extension-retraction means 531 andsecond extension-retraction means 537 positioned to one side of firstextension-retraction means 531. The components of extension-retractionmeans 537 corresponding with those of extension-retraction means 533 areindicated in FIGS. 13 and 14 with like references numbers that areprimed. As shown, extension retraction means 531 comprises extension arm533 having a first end 649 which is maintained, during the operation ofextension-retraction means, in sliding compartment 650 (FIG. 11).Extension arm 533 includes second end 651 pivotably secured betweenupper and lower plates 547, 549 of main body 534. Connector member 653is secured to arm 531 at one end and secured (e.g. pivotably) tohydraulic cylinder 655 at its other end. Hydraulic cylinder 655 issecured (e.g. pivotably) at end 657 to a rigid portion of deck 522 suchthat arm 531 can be independently extended and retracted by hydraulicmember 655. A similar arrangement is provided for extension-retractionmeans 537.

As noted, extension-retraction means 533 and 537 are extendable andretractable independent of one another. Thus, main body 532 can beangled by extending or retracting one extension-retraction means furtherthan the other. Swing slot 647 is provided in upper plate 590 and asimilarly shaped end positioned slot (not shown) is formed in lower pate592. Pin member 647' is slidingly retained within the swing slots 647and passes through end 651' of arm 533' so as to enable the angling ofmain body 532.

FIGS. 11, 15 and 16 illustrate first exterior roller system 608 mountedon first lateral extension 544. First exterior roller system 608includes first roller assembly 609 and second roller assembly 610 whichare mounted on opposite sides of support beam 552. First roller assembly609 includes roller 611 pivotably supported on lever assembly 612. Firstsupport bracket 613 extends from one side of beam 552 and supportsroller 611 and lever assembly 612. To maintain lever assembly 612 androller 611 in position with respect to support bracket 613, a pair ofdisengageable engagement members 614 and 615 are provided.

Engagement member 614 includes spring biased pins similar to thosepreviously discussed in FIG. 17A. Engagement member 614 is activated toinsert the spring biased pins associated therewith through aligned holesin lever assembly 612 to lock roller 611 in an up position. When theroller is to be placed in a down or retracted position, engagementmember 614 is disengaged such that lever assembly is free to pivot aboutpivot members 616 and 617 (FIG. 14). Once in its down position,engagement member 615 is activated so as to insert pins through thealigned holes in lever assembly 612 previously occupied by the pins ofengagement member 614.

With reference to FIGS. 15 and 16, an exterior roller system 608' isshown which is similar to exterior roller system 608 and shows likecomponents with equivalent dashed reference numbers. FIG. 16 representsa side view of that which is shown in FIG. 15 and thus together withFIG. 11 provides a good illustration of second exterior roller assembly610' which includes bracket 618' supported by support beam 564 and lever623'. Lever 623' pivotably supports roller 622' and is pivotably joinedto bracket 618' by pivot pin 620'. Engagement member 619' (similar toarrangement of 614 and 615) extends through aligned holes in bracket618' to maintain roller 622' in the illustrated up position. To placeroller assembly 610' in a down position, engagement member 618' isdisengaged and lever 623' pivots down, until the pins of engagementmember 618' line up with holes 621' formed in bracket 618'.

FIG. 15 illustrates interior roller assemblies 625 and 625' mounted onmain body 534. Interior roller assemblies 625 and 625' are arranged onmain body 534 in the same fashion as that described for first rollerassemblies 609 and 609' which are mounted on the lateral extensions.

FIG. 12 illustrates first power roller assembly 627 and second powerroller assembly 628. First power roller assembly 627 includes powerroller 629 having axle 630 with gear 631 fixed thereto. Axle 630 isretained at one end within a notch formed in bracket 632 and at itsother end in an aperture formed in main body 534. Bracket 632 ispivotably secured to hydraulic system 633 which includes hydrauliccylinder 643 and fixed extension 644 which is supported by the deckstructure at one end and pivotably supports hydraulic cylinder 643 atits opposite end. Bracket 632 also supports motor 634 with driving shaft635 and gear 636.

Chain 637 extends to gear 638 formed on shaft 639. Shaft 639 pivotablysupports bracket 632 and has its adjacent end rotatably supported bymain body 534. Shaft 639 supports an additional gear (not shown) on theopposite side of bracket 632 which is in driving engagement with gear631 by way of a chain or intermediate gears (not shown).

Shaft 639 extends along a recess formed along the length of main body534 and is rotatably supported at its opposite end by main body 534.Shaft 639 also supports at its opposite end bracket 640. Power roller641 has a central axle (not shown) supported at one end by bracket 640and at its opposite end by main body 534. A second hydraulic system 633'is provided and has hydraulic cylinder 643' and extension 644' similarlyarranged to that of hydraulic system 633.

Shaft 639 includes a gear (not shown) at its end supported by bracket640 which powers roller 641 through the output of motor 643 supported onbracket 632.

By extending hydraulic cylinders 643 and 643', brackets 632 and 640pivot about shaft 639 to raise rollers 629 and 641 into a lifted,operating position and, by retracting hydraulic cylinder, rollers 629and 641 are placed in a lowered, stowage mode.

FIGS. 19A-25 illustrate another embodiment of the present inventionwhich is particularly suited for the transport of heavy cargo indifficult to reach loading bays and is especially suited for properpositioning of a primary and secondary interface without the need for ahigh degree of operator expertise. FIG. 19A shows a planar view ofinterface system 1000 which includes deck structure 1002 and interfaceassembly 1004. Deck structure 1002 includes an upper surface 1006 havinga plurality of non-powered rollers 1008 and a plurality of poweredrollers 1010 with the latter preferably being powered and positionablein the same way as the previously described embodiments.

As shown in FIG. 19A interface assembly 1004 includes primary interface1012 and secondary interface 1014. Primary interface 1012 features mainbody 1016 and roller 1018 (powered or non-powered) positioned in themidsection of main body 1016 and a pair of non-powered rollers 1019 atthe extremities of main body 1016. Main body 1016 has slot 1020 formedto one side of roller 1018.

Secondary interface 1014 includes main body 1026 which includes a pairof non-powered rollers 1028 spaced along the upper surface of main body1026.

Interface assembly 1004 further includes primary extension-retractionmeans 1022 and secondary extension-retraction means 1024. Primaryextension-retraction means 1022 includes first primary arm 1030 andsecond primary arm 1032. First primary arm 1030 includes pin 1034 whichis slidingly and pivotably received within slot 1020. Second primary arm1032 includes pin 1036 at its external end and pin 1036 pivotably fixesthe external end of arm 1032 to main body 1016.

Secondary extension-retraction means 1024 includes first secondary arm1038 and second secondary arm 1040. Secondary arm 1040 is pivotablysecured to main body 1026 at the end thereof and main body 1026 includesslot 1027 formed at one end which receives in sliding fashion pin 1029provided at the end of secondary arm 1038. Secondary arms 1038 and 1040are also positioned laterally outside of primary arms 1030 and 1032.

FIG. 19A shows in solid lines arms 1030 and 1032 of primaryextension-retraction means 1022 in their most extended position and arms1038 and 1040 of secondary extension-retraction means 1024 in their mostextended position. FIG. 19A also shows in dashed lines the angledorientation of main bodies 1016 and 1026 when arms 1032 and 1040 are attheir maximum extension and arms 1030 and 1038 are near or at theirminimum retraction.

FIG. 19A further illustrates deck width W1 (e.g., 108 inches), width W2of main body 1016 (e.g., 90 inches) and width W3 of main body 1026(e.g., 58 inches). With width W1 of deck structure 1002 being thewidest, the lesser width of main body 1016 is more easily reachable intocertain limited spaces associated with cargo bays. Moreover, theintermediate or secondary main body 1026 is positioned so as tofacilitate the continued support of cargo as the cargo is passed fromthe front edge of primary interface 1012 to the front end of deckstructure 1002 which is a length L1 (e.g., 24-32 inches). Main body 1026of secondary interface 1014 is positioned essentially half-way orintermediately (e.g., 12-16 inches) between the front end of deckstructure 1002 and main body 1016 (i.e. L1/L2=2).

FIG. 19B shows a side view of that which is shown in FIG. 19A. As shownin FIGS. 19A and 19B, main body 1026 has a through-area through whicharms 1030 and 1032 extend. The through-area through which arms 1030 and1032 extend can be lined with low-friction bearing surfaces (e.g.brass). Arms 1038 and 1040 are secured within main body 1026 in betweenthe upper and lower surface of main body 1026. FIG. 19B also illustratesthat powered rollers 1018 and 1010 are at the same level whilenon-powered rollers 1028, 1019 and 1008 are also at the same level. Theupper surface of deck structure 1002 is also level with the uppersurface of the primary and secondary interfaces.

FIG. 20 illustrates a planar view like that in FIG. 19A except with theupper surface of deck 1002 removed for clarity and primaryextension-retraction means 1022 and secondary extension-retraction means1024 in their retracted position.

As shown in FIG. 20, deck structure 1002 includes frame substructure1042 upon which arms 1030 and 1032 are supported in sliding fashion. Toensure arms 1030 and 1032 remain parallel to one another and transverseto the front end of deck 1002, roller guides 1044 are provided. In apreferred embodiment, guides 1044 are cylindrical rollers extendingbetween substructure 1042 and the upper plate surface 1046 of deck 1002(FIG. 19B). Frame substructure 1042 is preferably rectangular in shapeand is joined at its exterior sides to upper plate 1046 by transverselyextending side plates one of which is represented by 1048 in FIG. 19B.

Arms 1030 and 1032 are quadrilateral in cross-section (see FIG. 22) andinclude a hollow recess along their entire length. Arm 1030 includesinternal end 1050 and arm 1032 includes internal end 1052 which arecoplanar when the primary and secondary interfaces 1012 and 1014 are intheir retracted stowage mode. Received within the hollow internal end1050 of arm 1030 is first hydraulic assembly 1054. First hydraulicassembly 1054 is fixed at one end to arm 1032 and at its opposite end tobeam 1056 which, in turn, is fixed to substructure 1042. Secondhydraulic member 1057 is fixed at one end to arm 1032 and at itsopposite end to beam 1056.

Main bracket 1058 extends off of the interior side of arm 1032 towardsarm 1030. Main bracket 1058 includes pin 1065 which has a center portionwhich slides within slot 1062 formed in main plate 1064 and an upperflange 1066 which slides on main plate 1064 so as to further support andstabilize arm 1032. Main plate 1064 is secured (e.g., welded) to decksubstructure 1042.

FIGS. 20 and 21 illustrate first interplay means 1068 and secondinterplay means 1070. FIG. 21 illustrates in greater detail interplaymeans 1068 and the following description concerns interplay means 1068only as both interplay means 1068 and 1070 operate in the same manner.As shown in FIGS. 21 and 22, arm 1030 includes traversely extendingsecondary arm guide 1072. Guide 1072 is fixed at one end to the bottomof arm 1030. Also extending traversely off of the exterior side of arm1030 is securement bar 1074 which has first bracket 1076 fixed to chainor belt 1080 and flange 1078 bolted to arm 1030. Chain 1080 is wrappedabout first sprocket 1082 and second sprocket 1084 which are spacedalong and rotatably fixed to an upper surface of arm 1038.

While interface system 1000 is in the stowage mode, first bracket 1076is positioned close to second sprocket 1084 (e.g., one sprocket radiusaway from center of sprocket along the length of arm 1038). While in thestowage mode, a second bracket 1086 is also secured to chain 1080 onlyon the opposite (external) side of beam 1038. Second bracket 1086 isspaced from second sprocket 1084 at about the same distance as firstbracket 1076 is spaced from first sprocket 1082. Second bracket 1086 isfixed to first lateral plate 1088 (corresponding second lateral plate1090 is similarly arranged on the opposite side of deck 1002). First andsecond lateral plates 1088 and 1090 are fixed (e.g., welded) tosubstructure 1042.

Secondary arm 1038 is supported and guided by guiding beam 1092 which issupported at its ends to substructure 1042. FIG. 23 illustrates arm 1038received within recess 1094 formed in guiding beam 1092. To facilitatethe sliding of arm 1038, low friction bearing layer 1096 is provided.For further stability, Z-shaped brackets 1098 and 1100 are added so asto prevent vertical movement of secondary arm 1038. Alternatively, beam1092 can have a larger height with a central slot formed therein (notshown) with beam 1038 passing therethrough. With this latterarrangement, a clearance recess (not shown) can be provided to avoid anyabutment between primary arm 1030 and beam 1092.

The present invention also contemplates reliance on the guidanceprovided by guiding beam 1092 without relying on support 1072 (bothsides). Thus, with this arrangement each primary arm would include atransverse guide and beam 1092 would be removed. The present inventionalso contemplates the alternate arrangement wherein reliance is placedon support 1072 and not on guiding beam 1092.

FIG. 24 shows the arrangement of interface assembly 1004 when it is inits most extended position. As shown in FIG. 24, first hydraulics rod1102 and second hydraulics rod 1104 are extended to their maximum so asto place the end of arms 1038 and 1040 just prior to guide beam 1092.Moreover, center pin 1065 of main bracket 1058 is at the forward mostend of slot 1062.

In the most extended position, central axis 1106 of main body 1016 islength X away from front end 1110 of substrate 1042. Also, center axis1108 of main body 1026 is length X/2 away from front end 1110. As shownin FIG. 24, bracket 1086 and support bar 1074 have moved with chain 1080as chain 1080 rotated counterclockwise during the extension of primaryarm 1030.

Interplay means 1068 and 1070 thus act to coordinate and control themovement of primary and secondary interfaces 1012 and 1014 such that thecentral axis of interface 1012 is always essentially twice the distancefrom front end 1110 as interface 1014.

The general principle lying behind the coordinated movement of interface1012 and 1014 can be seen with reference to FIG. 26. In FIG. 26, pulleyP has its center rise, between time periods T₁ and T₂, a distance X/2when point S on belt R is moved a distance X. Weight W is used tomaintain tension in belt R which is fixed at one end to ceiling F. Inthe present invention fixed bracket 1086 provides the function ofceiling F discussed above while sprocket 1084 provides the function ofpulley P, chain 1080 the function of belt R and the frictional contactbetween arm 1038 and the supporting surface provides an effect similarto that of weight W.

FIG. 25 illustrates that the interplay means of the present inventionnot only halves the distance of extension for interfaces 1012 and 1014but also halves their angle of orientation. This arrangement isparticularly helpful in providing evenly distributed support to a loadbeing transferred between deck 1002 and a cargo bay. As shown in FIG.25, arm 1032 is fully extended as it was shown in FIG. 24. Arm 1030,however, is non-extended or only slightly extended from its stowageposition. Slots 1020 and 1027 and the associated pins 1029, 1034 providethe required play to handle the hypotenuse positionment of main bodies1016 and 1026. With this arrangement, horizontal line 1116 extendingthrough pivot pin 1112 forms an angle "0" with respect to central axis1106. Also, because of the interplay means 1068 and 1070, the angleformed between a line parallel to horizontal line 1118 and extendingthrough pivot 1114 and central axis 1108 is "θ/2".

Although the present invention has been described with reference topreferred embodiments, the invention is not limited to the detailsthereof. Various substitutions and modifications will occur to those ofordinary skill in the art, and all such substitutions and modificationsare intended to fall within the spirit and scope of the invention asdefined in the appended claims.

What is claimed is:
 1. An interface system for a cargo loader,comprising:first and second extension-retraction means positioned inspaced relationship with one another, and each having a first endadapted for connection with a deck of a cargo loader and a second end;and an interface assembly secured to the second end of said first andsecond extension-retraction means, said interface assembly having a mainbody with an upper and a lower surface and a first and a second end, thefirst end of said main body being pivotally secured to the second end ofsaid first extension-retraction means and the second end of said mainbody being pivotably secured to the second end of said secondextension-retraction means, a first lateral extension member having afirst end pivotably secured to the first end of said main body and asecond end, the first end of said first lateral extension member beingpivotably secured to said main body about an axis which extends betweenthe upper and lower surfaces of said main body, a second lateralextension member having a first end pivotably secured to the second endof said main body and a second end, and the first end of said secondlateral extension member being pivotally secured to said main body aboutan axis which extends between the upper and lower surface of said mainbody, first locking means for locking said first lateral extension in anextended position wherein said first lateral extension extends out awayfrom both said first and second extension-retraction means and a firstlocking assembly for locking said first lateral extension in a retractedposition wherein said first lateral extension extends out away from saidfirst extension-retraction means and towards said secondextension-retraction means, second locking means for locking said secondlateral extension in an extended position wherein said second lateralextension member extends out away from both said first and secondextension-retraction means and a second locking assembly for lockingsaid second lateral extension member in a retracted position whereinsaid second lateral extension extends out away from said secondextension-retraction means and towards said first extension-retractionmeans.
 2. An interface system as recited in claim 1 wherein said firstand second lateral extensions each include a support beam and said firstand second lateral extensions each include, at the first end, a bracketmember extending transverse to said support beam, said first and secondlocking means also each including a pivot pin secured to said main bodyand pivotably secured to said bracket member on one side of said supportbeam, said first and second locking means each comprising disengageableengagement means supported by said bracket member on an opposite side ofsaid support beam for releasably fixing said lateral extensions in theextended position, and said first and second locking assemblies eachfurther comprising a first lock member secured to a respective one ofsaid lateral extensions and a second lock member secured to said mainbody and said first and second lock members being dimensioned andarranged such that said lateral extensions are releasably locked by saidfirst and second lock members in the retracted position.
 3. An interfacesystem as recited in claim 2 further comprising exterior rollerassemblies positioned on each of said lateral extension members saidroller assemblies including rollers and releasable locking means which,when engaged, lock said rollers in a raised position and when disengagedresult in said rollers being freely pivotable to a lowered position. 4.An interface system as recited in claim 3 further comprising interiorroller assemblies positioned on said main body and including rollers andreleasable locking means which, when engaged, position said rollers in araised position and when disengaged, result in said rollers being freelypivotable to a lowered position.
 5. An interface cargo system as recitedin claim 2 wherein said disengageable engagement means includes acylinder supported by said bracket member and said cylinder having aslot extending axially therealong, a pair of engagement pins havinggripping means and positioned within said cylinder so as to have saidgripping means extending through said slot, and a spring positionedbetween said engagement pins to bias said pins outwardly.
 6. Aninterface system as recited in claim 1 further comprising exteriorroller assemblies positioned on each of said lateral extension members,said roller assemblies including rollers and releasable locking meanswhich, when engaged, lock said rollers in a raised position and whendisengaged result in said rollers being freely pivotable to a loweredposition.
 7. A interface system as recited in claim 6 further comprisinginterior roller assemblies positioned on said main body and includingrollers and releasable locking means which, when engaged, position saidrollers in a raised position and when disengaged, result in said rollersbeing freely pivotable to a lowered position.
 8. An interface cargosystem as recited in claim 1 further comprising a powered rollerassembly supported by said main body, said powered roller assemblyincluding rollers and means for driving said rollers and means forraising said rollers to a position above the upper surface of said mainbody and for lowering said rollers to a position below the upper surfaceof said main body.
 9. An interface system as recited in claim 1 whereinsaid first and second extension-retraction means each include anelongated arm and a hydraulic member connected at one end to said armand at an opposite end to the deck such that said first and second armsare independently extendable and retractable away and towards the deck.10. An interface system as recited in claim 9 wherein said main bodyincludes a plate with a slot, and said arm of said secondextension-retraction means is slidingly fixed within said slot such thatsaid main body is angled when said arms are extended away from the deckfor different lengths.
 11. An interface system as recited in claim 1wherein said main body includes a central axis extending between thefirst and second ends of said main body and wherein said locking meansis dimensioned and arranged such that said lateral extensions extend outessentially along the central axis of said main body when in theextended position and extend inwardly along an axis which is spaced andparallel to the central axis of said main body when in the retractedposition.
 12. An interface system as recited in claim 11 wherein saidlocking means and dimension are arranged such that said lateralextensions pivot essentially 180° in passing between said extendedposition and said retracted position.
 13. An interface assembly asrecited in claim 7 further comprising a powered roller assemblysupported by said main body, said powered roller assembly includinglaterally spaced rollers and means for driving said laterally spacedrollers and means for raising said rollers to a position above the uppersurface of said main body and for lowering said rollers to a positionbelow the upper surface of said main body.
 14. An interface assembly asrecited in claim 1 wherein said lateral extension members include asupport beam and a bracket member with the support beam and bracketmember arranged such that each lateral extension has a T-shapedcross-section along a horizontal bisecting plane.
 15. An interfaceassembly as recited in claim 14 wherein each of said support beamssupport a first and a second roller with the first roller being on oneside of the support beam and a second roller being on an opposite sideof said support beam and said first and second rollers being laterallyspaced along each of said support beams.
 16. An interior assembly asrecited in claim 15 further comprising interior roller assembliessupported by said main body such that each interior roller assembly ispositioned laterally outward of one of said rollers on said lateralextension members when said lateral extensions are in said retractedposition.
 17. An interface system for a cargo loader, comprising:a deckhaving a front end, an upper surface and a bottom surface, and said deckhaving a storage compartment formed in the upper surface and at thefront end of said deck; first and second extension-retraction meanspositioned in spaced relationship with each other and each having afirst end supported by said deck and a second end; an interface assemblysecured to the second end of said first and second extension-retractionmeans, said interface assembly including, a main body secured to saidfirst and second extension-retraction means, said main body having anupper and a lower surface and a first and second end, a first lateralextension member pivotably secured to the first end of said main body,said first lateral extension being adapted to rotate about an axisextending between the upper and lower surface of said main body, asecond lateral extension member pivotably secured to the second end ofsaid main body, said second lateral extension being adapted to rotateabout an axis extending between the upper and lower surface of said mainbody, first locking means for locking said first lateral extension in anextended position wherein said first lateral extension extends away fromboth said first and second extension-retraction means and a firstlocking assembly for locking said first lateral extension in a retractedposition wherein said first lateral extension extends out away from saidfirst extension-retraction means and towards said secondextension-retraction means, second locking means for locking said secondlateral extension in an extended position wherein said second lateralextension extends away from both said first and second extensionretraction means and a second locking assembly for locking said secondlateral extension in a retracted position wherein said second lateralextension extends away from said second extension-retraction means andtowards said first extension-retraction means.
 18. An interface systemas recited in claim 17 wherein said first and secondextension-retraction means each include an elongated arm pivotablysecured at one end to said main body and slidingly received within anelongated recesses formed in said deck.
 19. An interface system asrecited in claim 18 wherein said extension-retraction means includesliding means for sliding said arms within said elongated recesses, andwherein said arms and said corresponding recesses are dimensioned andarranged so as to limit movement of said arms to sliding travel solelyalong a central axis of said elongated recesses.
 20. An interface systemas recited in claim 19 wherein said main body includes a slotted platewithin which a second end of the arm of said second extension-retractionmember is slidingly retained, and said arms being independently slidableby said sliding means so as to angle said interface assembly.
 21. Aninterface system as recited in claim 17 wherein said lateral extensionmembers include a support beam with a first side, and first and secondroller assemblies positioned on the first side of a respective one ofsaid support beams, said main body including a recessed front sectionand third and fourth roller assemblies supported by said main body andspaced along the recessed front section of said main body, and saidfirst and second roller assemblies including rollers having an axis ofrotation which is common with the axis of rotation of rollers of saidthird and fourth roller assemblies when said lateral extension membersare in the retracted position.
 22. An interface assembly for a cargoloader, comprising:a first and a second extension-retraction assemblypositioned in spaced relationship with respect to each other, and eachextension-retraction assembly having a first end adapted for connectionwith a cargo loader and a second end; and an interface assembly having amain body pivotably secured to the second end of said first and saidsecond extension-retraction assembly, a first lateral extension memberpivotably supported by a first end of said main body, said first lateralextension including a support beam and a bracket member joined to oneend of said support beam and extending transverse to said support beamso as to form a T-shaped combination, and one end of said bracket memberbeing pivotably secured to said one end of said main body such that saidfirst lateral extension is adapted for pivoting movement between aretracted position wherein said support beam is juxtaposed to a frontend of said main body and an extended position wherein said support beamextends laterally out away from said main body, a second lateralextension member pivotably supported by a second end of said main body,said second lateral extension including a support beam and a bracketmember joined to one end of said support beam and extending transverseto said support beam so as to form a T-shaped combination, and one endof said bracket member of said second lateral extension being pivotablysecured to the second end of said main body such that said secondlateral extension is adapted for pivoting movement between a retractedposition wherein the support beam of said second lateral extension isjuxtaposed to a front end of said main body to a second position whereinthe support beam of said second lateral extension laterally extends outaway from said main body, a first locking assembly for locking saidfirst lateral extension in the extended position, said first lockingassembly being dimensioned and arranged so as to releasably fix thebracket member of said first lateral extension to said main body, and asecond locking assembly for locking said second lateral extension in theextended position, said second locking assembly being dimensioned andarranged so as to releasably fix the bracket members of said secondlateral extension member to said main body.
 23. An interface system asrecited in claim 22 wherein said first and second locking assembliesengage an end of said bracket member which is opposite to the endpivotably secured to said main body.
 24. An interface system as recitedin claim 22 wherein said support beam of said first and second lateralextension members, includes a roller assembly.